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    An Alternative Analysis of the Plane Stick-Slip Problem

    Source: Journal of Applied Mechanics:;1983:;volume( 050 ):;issue: 4a::page 863
    Author:
    A. Dutta
    DOI: 10.1115/1.3167158
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The plane stick-slip problem has been solved analytically using the separation of variable technique. The essence of the mathematical procedure is to solve the problem separately for the “stick” and the “slip” regions and then to match the two solutions at the exit plane. The present solution, which is relatively easy to evaluate, yields results that compare favorably with those obtained by the Wiener-Hopf technique. Furthermore, the stick-slip solution has been used to estimate the expansion of a two-dimensional plane Newtonian jet at very low Reynolds numbers. For capillary numbers less than 0.1, the approximate method predicts swell ratios that are in fairly good agreement with those obtained from a more elaborate numerical solution of the jet swell problem.
    keyword(s): Stick-slip , Separation (Technology) AND Reynolds number ,
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      An Alternative Analysis of the Plane Stick-Slip Problem

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    contributor authorA. Dutta
    date accessioned2017-05-08T23:14:35Z
    date available2017-05-08T23:14:35Z
    date copyrightDecember, 1983
    date issued1983
    identifier issn0021-8936
    identifier otherJAMCAV-26226#863_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/96559
    description abstractThe plane stick-slip problem has been solved analytically using the separation of variable technique. The essence of the mathematical procedure is to solve the problem separately for the “stick” and the “slip” regions and then to match the two solutions at the exit plane. The present solution, which is relatively easy to evaluate, yields results that compare favorably with those obtained by the Wiener-Hopf technique. Furthermore, the stick-slip solution has been used to estimate the expansion of a two-dimensional plane Newtonian jet at very low Reynolds numbers. For capillary numbers less than 0.1, the approximate method predicts swell ratios that are in fairly good agreement with those obtained from a more elaborate numerical solution of the jet swell problem.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Alternative Analysis of the Plane Stick-Slip Problem
    typeJournal Paper
    journal volume50
    journal issue4a
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3167158
    journal fristpage863
    journal lastpage868
    identifier eissn1528-9036
    keywordsStick-slip
    keywordsSeparation (Technology) AND Reynolds number
    treeJournal of Applied Mechanics:;1983:;volume( 050 ):;issue: 4a
    contenttypeFulltext
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